A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers

A. Fatsis,; A. Panoutsopoulou,; N. Vlachakis,; V.N. Vlachakis,

doi:10.1515/TJJ.2006.23.1.15

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A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers

A. Fatsis, , A. Panoutsopoulou, , N. Vlachakis, and V.N. Vlachakis,

Published/Copyright: March 1, 2006

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From the journal International Journal of Turbo and Jet Engines Volume 23 Issue 1

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Harvard
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Fatsis,, A., Panoutsopoulou,, A., Vlachakis,, N. and Vlachakis,, V.N.. "A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers" International Journal of Turbo and Jet Engines, vol. 23, no. 1, 2006, pp. 15-26. https://doi.org/10.1515/TJJ.2006.23.1.15

Fatsis,, A., Panoutsopoulou,, A., Vlachakis,, N. & Vlachakis,, V. (2006). A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers. International Journal of Turbo and Jet Engines, 23(1), 15-26. https://doi.org/10.1515/TJJ.2006.23.1.15

Fatsis,, A., Panoutsopoulou,, A., Vlachakis,, N. and Vlachakis,, V. (2006) A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers. International Journal of Turbo and Jet Engines, Vol. 23 (Issue 1), pp. 15-26. https://doi.org/10.1515/TJJ.2006.23.1.15

Fatsis,, A., Panoutsopoulou,, A., Vlachakis,, N. and Vlachakis,, V.N.. "A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers" International Journal of Turbo and Jet Engines 23, no. 1 (2006): 15-26. https://doi.org/10.1515/TJJ.2006.23.1.15

Fatsis, A, Panoutsopoulou, A, Vlachakis, N, Vlachakis, V. A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers. International Journal of Turbo and Jet Engines. 2006;23(1): 15-26. https://doi.org/10.1515/TJJ.2006.23.1.15

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Published Online: 2006-03

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Articles in the same Issue

CONTENTS
Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor

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https://doi.org/10.1515/TJJ.2006.23.1.15

Articles in the same Issue

CONTENTS
Numerical Investigation of Unsteady Flow in a Low Pressure Turbine
A 3D Simulation of Unsteady Flow Inside Centrifugal Compressor Impellers
Numerical Research on the Three Dimensional Unsteady Flow within the Vortex Pump
Variational Principle for 3-D Steady Rotational Flow in Rotor Using Two Stream Functions
Effect of Exit Geometry on the Flow Characteristic of Jet Exhausts
Effects of the Inlet Boundary Layer Thickness on the Loss Characteristics in an Axial Compressor